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LEMUR-2-WOBLER

In orbit NORAD 67368 UYAO-5268-1897-4403-3475

Observations 0
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Falcon 9 Block 5 | Pandora / Twilight rideshare mission

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

0

Observations all time

Mission information
Spacecraft name
LEMUR-2-WOBLER
Status
Active
The satellite is in orbit
The network has not received data from this satellite for a long time
Launch and timeline
Launch
Falcon 9 Block 5 | Pandora / Twilight rideshare mission
Carrier rocket
Falcon 9 Block 5
Spaceport
Space Launch Complex 4E
Launch time
Separation time
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
590.77 km
Apogee
604.10 km
Inclination
97.8°
Period
96.7 min
Semi-major axis
6975.6 km
Velocity
7.56 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-13 06:09:06 UTC
Two-line elements (TLE)
1 67368U 26004F   26285.92180737  .00003562  00000-0  38211-3 0  9996
2 67368  97.8114 282.9505 0009550 101.5862 258.6427 14.89213373 40813
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Orbit history, past year

Mean elements of every TLE set over the past 365 days, plotted against the epoch of the set. Each source is its own line; click it in the legend to hide it. A jump in altitude is a manoeuvre or a bad set; lines drifting apart are a disagreement between sources. “TLE age” is how many hours have passed since the epoch of the source's freshest set, plotted against when the set reached us, on a logarithmic scale. A set the source repeats unchanged does not reset the age.

Prediction divergence

Each TLE set is propagated with SGP4 to the epoch of the next set from the same source and compared with it, plotted against the epoch of the next set; the tooltip shows how many hours ahead the prediction ran. The logarithmic scale shows the size of the divergence and the tooltip its sign: plus along-track means the prediction is ahead of the satellite. This is how well the sets agree, not the true error: the reference is a TLE too, off by about a kilometre. An outlier is a manoeuvre between sets. Sets more than a week apart are not compared.

Time of closest approach, UTC Object 1 Object 2 Distance, km Speed, km/s Max. probability
2026-10-13 21:08:28 LEMUR-2-WOBLER
NORAD 67368 		POSIDONIA
NORAD 69922 		2.224 11.33 6.3e-07
2026-10-14 01:58:43 LEMUR-2-WOBLER
NORAD 67368 		GRUS-3D
NORAD 69919 		2.619 11.33 4.6e-07
2026-10-14 04:41:37 CATCH-1
NORAD 60088 		LEMUR-2-WOBLER
NORAD 67368 		4.901 13.29 1.0e-07
2026-10-14 14:52:54 LEMUR-2-WOBLER
NORAD 67368 		GEMINI-POLLUX
NORAD 69000 		4.777 11.64 1.3e-07
2026-10-15 19:51:57 LEMUR-2-WOBLER
NORAD 67368 		SL-14 R/B
NORAD 14552 		4.775 14.97 1.7e-07
2026-10-15 23:48:14 LEMUR-2-WOBLER
NORAD 67368 		FENGYUN 1C DEB
NORAD 31443 		2.015 13.91 5.4e-07
2026-10-16 17:20:47 LEMUR-2-WOBLER
NORAD 67368 		COSMOS 2251 DEB
NORAD 37126 		2.999 15.08 1.7e-07
2026-10-18 04:15:17 LEMUR-2-WOBLER
NORAD 67368 		CZ-4B DEB
NORAD 26262 		4.320 12.17 1.5e-07
2026-10-18 10:30:46 AEROCUBE 6A
NORAD 40045 		LEMUR-2-WOBLER
NORAD 67368 		1.185 14.91 1.2e-06
2026-10-18 22:04:56 LEMUR-2-WOBLER
NORAD 67368 		GRUS-3B
NORAD 69918 		2.917 11.33 3.7e-07
2026-10-19 02:55:11 LEMUR-2-WOBLER
NORAD 67368 		SPEAR-1C
NORAD 69897 		4.260 11.34 1.7e-07

Data: CelesTrak SOCRATES Plus, computed from TLEs of the public catalog. This is an estimate, not grounds for a manoeuvre: TLEs carry no covariance, and the maximum probability assumes a position error.

All conjunctions of this satellite